EP1676148A1 - System and method for protecting means of transport from ir-guided missiles - Google Patents
System and method for protecting means of transport from ir-guided missilesInfo
- Publication number
- EP1676148A1 EP1676148A1 EP04802633A EP04802633A EP1676148A1 EP 1676148 A1 EP1676148 A1 EP 1676148A1 EP 04802633 A EP04802633 A EP 04802633A EP 04802633 A EP04802633 A EP 04802633A EP 1676148 A1 EP1676148 A1 EP 1676148A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- laser array
- warning device
- missile warning
- transport
- laser
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/48—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
- G01S7/495—Counter-measures or counter-counter-measures using electronic or electro-optical means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/22—Homing guidance systems
- F41G7/224—Deceiving or protecting means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H13/00—Means of attack or defence not otherwise provided for
- F41H13/0043—Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target
- F41H13/005—Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target the high-energy beam being a laser beam
- F41H13/0056—Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target the high-energy beam being a laser beam for blinding or dazzling, i.e. by overstimulating the opponent's eyes or the enemy's sensor equipment
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/48—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
- G01S7/4804—Auxiliary means for detecting or identifying lidar signals or the like, e.g. laser illuminators
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/48—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
- G01S7/481—Constructional features, e.g. arrangements of optical elements
Definitions
- the invention relates to a system and a method for the protection of means of transport against IR-guided missiles according to the preambles of claims 1 and 12.
- a disadvantage of the weapon systems in which IR radiation is directed onto the attacking missiles by means of lamps is the high weight and the large volume of the system. Further disadvantages are the low efficiency of the system due to a low interference-to-signal ratio and the high power consumption. In the laser DIRCM weapon systems so-called trackers are usually required to track the attacking missiles, which makes the construction of the system expensive.
- the system according to the invention is characterized in that a laser array for disturbing the IR-guided missile is coupled to the missile warning device.
- the laser array comprises a number, usually several hundred, of laser diodes.
- the laser diodes advantageously operate with a wavelength in the range of 2-5 microns, wherein suitably laser diodes are used with an output power of 1 KW / cm 2 at a temperature of 300K.
- the laser diodes in their wavelength range.
- a first part of the laser diodes covers a wavelength range of 2-3.5 ⁇ m and a second part of the laser diodes covers the wavelength range of 3.5-5 ⁇ m.
- the two types of laser diodes can be arranged arbitrarily or according to a predeterminable pattern on the laser diode array.
- the laser array comprises diode-pumped semiconductor lasers or diode-pumped disk lasers or diode-pumped semiconductor wafer lasers.
- the laser array comprises diode-pumped semiconductor lasers or diode-pumped disk lasers or diode-pumped semiconductor wafer lasers.
- the sole FIGURE shows the system according to the invention in an exemplary basic representation.
- the reference symbol G designates the housing which encloses the system components, in particular the missile warning device F, the laser array LA arranged on a joint GK, the power supply SV and cooling systems KS and the data processing unit DV.
- Another system, not shown, which is located in the housing G, is an image sensor for reading the data from the sensor heads SK of the missile warning device F.
- means (not shown) are provided with which the housing G to the Shell of an aircraft FL can be attached.
- the missile WAM device F is advantageously aligned in a predeterminable spatial direction.
- the field of view SF of the missile warning device F advantageously covers a solid angle of 90 °.
- the spatial direction of the line of sight of the missile warning device depends in particular on which position of the aircraft the system according to the invention is attached.
- the missile warning device F is aligned in a system which is provided for example for installation at the bow of the aircraft at 45 ° to the direction of flight.
- the missile warning device F in a system which is provided, for example, for installation on the underside of the aircraft, is preferably oriented at 90 ° to the flight direction. This ensures that with a number of eg 4-6 systems, the entire environment of an aircraft can be covered by the sensors.
- the effective field WF of the laser array LA is greater than or equal to the field of view SF of the missile warning device F. This ensures that the effective fields WF cover several systems mounted on the aircraft, thereby ensuring a higher efficiency of the defensive measures. In addition, it is thus possible to simultaneously disturb a plurality of objects identified in the field of view SF of the missile warning device F and possibly identified as a threat.
- the sensor heads SK of the missile warning device F sweep over a field of view SF, in which the signal of an approaching object (not shown) can be detected.
- the signals of the sensor heads SK of the missile warning device F are read out by the image sensor and further processed for identification and tracking of the detected object.
- the evaluation of the exhaust gas jet of the approaching object in particular takes place taking into account definable parameters, e.g. Temperature, length. This information is compared by the system according to the invention with the behavior of an attacking rocket, whereby a statement can be made as to which threat emanates from the approaching object against the aircraft to be protected.
- a warning signal is sent to the data processing unit DV.
- This warning signal expediently includes precise details of the attacking object, in particular the height and the azimuth direction.
- the data processing unit DV is expediently a tactical computer which continues the tracking of the object.
- the sensor heads SK of the missile warning device F identify several objects as a threat.
- several warning signals are sent to the data processing unit DV, which sorts possible defenses regarding the relevance of the threat.
- the data processing unit DV calculates the direction of the object to be defended.
- the line of sight of the laser array LA is aligned in this direction.
- the alignment of the laser array LA is advantageously carried out by means of the joint GK on which the laser array LA is arranged.
- the joint GK is mounted with two axes (not shown). This ensures that the line of sight of the laser array LA can be aligned quickly and reliably in any spatial direction.
- a laser beam in particular a modulated laser beam, is emitted in the predetermined direction with the laser array LA.
- the line of sight of the laser array is already aligned in the direction of a detected object before it is eventually identified as a threat.
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL04802633T PL1676148T3 (en) | 2003-10-25 | 2004-10-21 | System and method for protecting means of transport from ir-guided missiles |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10349869A DE10349869A1 (en) | 2003-10-25 | 2003-10-25 | System and method for protecting means of transport against IR-guided missiles |
PCT/DE2004/002345 WO2005045465A1 (en) | 2003-10-25 | 2004-10-21 | System and method for protecting means of transport from ir-guided missiles |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1676148A1 true EP1676148A1 (en) | 2006-07-05 |
EP1676148B1 EP1676148B1 (en) | 2008-11-26 |
Family
ID=34559201
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP04802633A Not-in-force EP1676148B1 (en) | 2003-10-25 | 2004-10-21 | System and method for protecting means of transport from ir-guided missiles |
Country Status (7)
Country | Link |
---|---|
US (1) | US20080088496A1 (en) |
EP (1) | EP1676148B1 (en) |
AT (1) | ATE415637T1 (en) |
DE (2) | DE10349869A1 (en) |
ES (1) | ES2318355T3 (en) |
PL (1) | PL1676148T3 (en) |
WO (1) | WO2005045465A1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2887327B1 (en) * | 2005-06-17 | 2007-08-24 | Thales Sa | METHOD FOR THE PROTECTION OF ANTIMISSIL VEHICLES AND DEVICE FOR IMPLEMENTING THE SAME |
KR20090031346A (en) * | 2006-04-10 | 2009-03-25 | 엘타 시스템즈 리미티드 | Distributed jammer system |
US8376277B2 (en) * | 2006-10-04 | 2013-02-19 | The Boeing Company | Large aircraft self-defense system installation configuration |
DE102007022820B4 (en) | 2007-05-15 | 2013-10-02 | Eads Deutschland Gmbh | IR deception system for the defense of missiles with IR-sensitive seekers |
US7961133B2 (en) * | 2007-11-15 | 2011-06-14 | Raytheon Company | System and method for diverting a guided missile |
FR2923915B1 (en) * | 2007-11-16 | 2009-11-27 | Thales Sa | IR SENSOR INTERFERENCE AND DAMAGE SYSTEM |
US8305252B2 (en) * | 2009-08-14 | 2012-11-06 | The United States Of America As Represented By The Secretary Of The Navy | Countermeasure device for a mobile tracking device |
US8665421B1 (en) * | 2010-04-19 | 2014-03-04 | Bae Systems Information And Electronic Systems Integration Inc. | Apparatus for providing laser countermeasures to heat-seeking missiles |
DK3514477T3 (en) * | 2018-01-22 | 2021-05-31 | Hensoldt Sensors Gmbh | SYSTEM AND METHOD FOR DISTURBING A TARGET POINT |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19938398A1 (en) | 1998-05-12 | 2002-09-19 | Hoesel Holger | Interference and measurement disruption system for defeating laser ranging- and speed-measurement of objects, uses optical interference signals radiated in direction of laser measurement system |
US6903674B2 (en) | 1999-05-07 | 2005-06-07 | Holger Hösel | Procedure and arrangement for jamming laser measuring instruments |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0237812A3 (en) * | 1986-03-20 | 1988-06-29 | Siemens Aktiengesellschaft | Semiconductor laser array with a collimated beam |
DE3833635A1 (en) * | 1988-10-04 | 1990-04-05 | Messerschmitt Boelkow Blohm | LASER WARNING RECEIVER |
FR2711806B1 (en) * | 1990-07-23 | 1995-12-29 | Aerospatiale | Detection and response system to an air threat. |
JPH0772680B2 (en) * | 1992-02-05 | 1995-08-02 | 防衛庁技術研究本部長 | Proximity protection device |
DE4402855C2 (en) * | 1994-01-31 | 1996-02-29 | Diehl Gmbh & Co | Defense device for an attacking target airborne missile |
DE4430830C2 (en) * | 1994-01-31 | 2003-06-26 | Diehl Stiftung & Co | Device for defense against an air target missile attacking an aircraft |
DE4444635C2 (en) * | 1994-12-15 | 1996-10-31 | Daimler Benz Aerospace Ag | Self-defense device against missiles |
US5742384A (en) * | 1996-05-02 | 1998-04-21 | Lockheed Martin Corporation | Compact scanning infrared countermeasure emitter |
EP0844495A1 (en) * | 1996-11-26 | 1998-05-27 | Matra Defense | Device for the detection of optical elements aimed at it |
US5909296A (en) * | 1997-04-04 | 1999-06-01 | The United States Of America As Represented By The Secretary Of The Air Force | Effective wide angle beam steering using spherical laser diode arrays |
DE19745785C2 (en) * | 1997-10-16 | 2002-12-05 | Eads Deutschland Gmbh | Laser radiation source for a DIRCM weapon system |
GB9804547D0 (en) * | 1998-03-05 | 2000-02-23 | Borrell Robert A | Weapons decoy |
US6244728B1 (en) * | 1999-12-13 | 2001-06-12 | The Boeing Company | Light emitting diode assembly for use as an aircraft position light |
DE10032698A1 (en) * | 2000-07-05 | 2002-01-17 | Schrodt Stephan | Directed high energy electromagnetic radiation detection system for mines, pipes and structures in earth, emits focused, penetrating, heating radiation, and returned radiation is analyzed |
DE10204397A1 (en) * | 2001-02-02 | 2002-08-22 | Optolab Licensing Gmbh | Laser diode array has each diode fitted to intermediate carrier mounted on base body acting as heat sink |
US6724792B2 (en) * | 2002-09-12 | 2004-04-20 | The Boeing Company | Laser diode arrays with replaceable laser diode bars and methods of removing and replacing laser diode bars |
US6977598B2 (en) * | 2003-03-07 | 2005-12-20 | Lockheed Martin Corporation | Aircraft protection system and method |
US6929214B2 (en) * | 2003-07-22 | 2005-08-16 | Northrop Grumman Corporation | Conformal airliner defense (CAD) system |
-
2003
- 2003-10-25 DE DE10349869A patent/DE10349869A1/en not_active Withdrawn
-
2004
- 2004-10-21 EP EP04802633A patent/EP1676148B1/en not_active Not-in-force
- 2004-10-21 PL PL04802633T patent/PL1676148T3/en unknown
- 2004-10-21 WO PCT/DE2004/002345 patent/WO2005045465A1/en active Application Filing
- 2004-10-21 AT AT04802633T patent/ATE415637T1/en not_active IP Right Cessation
- 2004-10-21 ES ES04802633T patent/ES2318355T3/en active Active
- 2004-10-21 DE DE502004008550T patent/DE502004008550D1/en active Active
- 2004-10-21 US US10/576,928 patent/US20080088496A1/en not_active Abandoned
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19938398A1 (en) | 1998-05-12 | 2002-09-19 | Hoesel Holger | Interference and measurement disruption system for defeating laser ranging- and speed-measurement of objects, uses optical interference signals radiated in direction of laser measurement system |
US6903674B2 (en) | 1999-05-07 | 2005-06-07 | Holger Hösel | Procedure and arrangement for jamming laser measuring instruments |
Also Published As
Publication number | Publication date |
---|---|
WO2005045465A1 (en) | 2005-05-19 |
ATE415637T1 (en) | 2008-12-15 |
DE502004008550D1 (en) | 2009-01-08 |
DE10349869A1 (en) | 2005-06-16 |
PL1676148T3 (en) | 2009-04-30 |
ES2318355T3 (en) | 2009-05-01 |
EP1676148B1 (en) | 2008-11-26 |
US20080088496A1 (en) | 2008-04-17 |
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